发明名称 |
Canted solar array and method for using same |
摘要 |
A method and apparatus for deploying a fixed and canted solar array of a satellite. The solar array is rotated in a first plane and about a first axis from a stowed position to a first position, rotated about a second axis orthogonal to the first axis from the first position to a deployed position determined by a deployment orbit of the satellite, and locked in the deployed position to prevent further motion of the solar array relative to a satellite body for the operational life of the satellite.
|
申请公布号 |
US2008078885(A1) |
申请公布日期 |
2008.04.03 |
申请号 |
US20060521672 |
申请日期 |
2006.09.15 |
申请人 |
CANTER STANLEY;FELLAND JANE R;FREIDHOFF DAVID P;NAKASONE DENNIS Y |
发明人 |
CANTER STANLEY;FELLAND JANE R.;FREIDHOFF DAVID P.;NAKASONE DENNIS Y. |
分类号 |
B64G1/44 |
主分类号 |
B64G1/44 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|